Author: National Aeronautics and Space Administration / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

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1231. NACA research memorandum RM (series). E52L02. Free-flight performance of rocket-boosted, air-launched 16-inch-diameter ram-jet engine at Mach numbers up to 2.20 [with list of references]; by John H. Disher, Robert C. Kohl, and Merle L. Jones.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Feb. 3, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1232. NACA research memorandum RM (series). E52J22. Characteristics of canard-type missile configuration with underslung scoop inlet at Mach numbers from 1.5 to 2.0 [with list of references]; by Evan A. Fredenburgh and Robert C. Campbell.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 30, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1233. NACA research memorandum RM (series). A52K07. Experimental investigation of applicability of hypersonic similarity law to bodies of revolution [with list of references]: by Stanford E. Neice and Thomas J. Wong.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 27, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1234. NACA research memorandum RM (series). L52K20. Summary of pitch-damping derivatives of complete airplane and missile configurations as measured in flight at transonic and supersonic speeds [with list of references]; by Clarence L. Gillis and Rowe Chapman, jr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 22, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1235. NACA research memorandum RM (series). L52K24. Wind-tunnel investigation to determine aerodynamic characteristics in steady roll of model at high subsonic speeds [with list of references]; by Richard E. Kuhn and James W. Wiggins.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 21, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1236. NACA research memorandum RM (series). E52E23. Effect of engine and control limits on steady-state and transient performance of turbojet engine with variable-area exhaust nozzle [with list of references]; by George Vasu and William L. Hinde.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 16, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1237. NACA research memorandum RM (series). A52.T31. Wind-tunnel investigation at subsonic and supersonic speeds of model of tailless fighter airplane employing low-aspect-ratio swept-baek wing-effects of external fuel tanks and rocket packets on drag characteristics [with list of references]; by Willard G. Smith.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, Jan. 12, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1238. NACA research memorandum RM (series). A52J30. Wind-tunnel investigation at subsonic and supersonic speeds of model of tailless fighter airplane employing low-aspect-ratio swept-back wing-stability and control [with list of references]; by Willard G. Smith.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 12, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1239. NACA research memorandum RM (series). E52J14. Effects of fuel temperature and fuel distribution on combustion efficiency of 16-inch ram-jet engine at simulated flight Mach number of 2.9 [with list of references]; by E. E. Dangle, A. J. Cervenka, and D. W. Bahr.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 8, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1240. NACA research memorandum RM (series). L52K10. Preliminary investigation of total-pressure-recovery characteristics of 15° semiangle movable-cone variable-geometry ram-jet inlet at free-jet Mach numbers of 1.62, 2.00, 2.53, and 3.05 [with list of references]; by Arthur H. Hinners, jr., and John B. Lee.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 8, 1953
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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